Invention Grant
- Patent Title: Exhaust systems and methods for gas turbine engine
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Application No.: US16215914Application Date: 2018-12-11
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Publication No.: US11255239B2Publication Date: 2022-02-22
- Inventor: Yoonshik Shin , Yogendra Yogi Sheoran , Daniel Brown
- Applicant: HONEYWELL INTERNATIONAL INC.
- Applicant Address: US NJ Morris Plains
- Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee Address: US NJ Morris Plains
- Agency: Lorenz & Kopf, LLP
- Main IPC: F01N1/08
- IPC: F01N1/08 ; F01D25/30 ; F02K1/38 ; F01N3/05 ; F02C7/14

Abstract:
A gas turbine engine includes a combustion section that generates combustive gases that form a primary exhaust flow and an exhaust system downstream from the combustion section. The exhaust system includes an eductor system that includes a body that extends along a first axis, and a plurality of ducts spaced apart about a circumference of the body. Each of the plurality of ducts define a plurality of eductor primary flow paths that terminate in a mixing chamber. The exhaust system includes a muffler system downstream from the mixing chamber that includes a plurality of baffles that cooperate to define a tortuous path and attenuate sound generated by the gas turbine engine. The exhaust system includes a housing that surrounds the eductor system and the muffler system such that the eductor system and the muffler system are contained within the housing.
Public/Granted literature
- US20190107020A1 EXHAUST SYSTEMS AND METHODS FOR GAS TURBINE ENGINE Public/Granted day:2019-04-11
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